04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10039722 EMBRAER GPX Ltda. (PC 722) ANAC STC NO. 2009S10-20 EMB-135BJ The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/or emissions levels of the original product areunchanged and remain appl none none 18.05.2012 10031622 EMBRAER S.A. EMB-500 01.09.2009 10032105 EMS AVIATION, Inc. REV. 1 FAA STC SR03333AT S-76A, S-76B, S-76C Installation of the Sky Connect Satellite Phone None Prior to installation of this modification it 21.09.2011 and Tracking System. must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 10038432 EMS AVIATION, Inc. FAA STC SR09583RC EC135 P1/P2/P2+/T1/T2/T2+ Installation of the Sky Connect Forte Iridium Satellite Phone and /orautomated reporting system (FAA STC SR09583RC) 10041017 EMS AVIATION, Inc. FAA STC NO SR02569NY AS 350 B,AS 350 B1,AS 350 B2 AS 350 B3,AS 350 BA,AS 350 D None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 16.02.2012 Installation of Sky Connect Tracking System This STC is not applicable to AS350B3 model If the holder agrees to permit another iaw Master Drawing ListMDL07094This STC is helicopters withmodification OP4305 (Arriel 2D person to use this certificate tomodify a the validation of FAA STC SR02569NY (last engine installation) incorporated. product, the holder must give to the other reissued April 15,2009) person writtenevidence of that permission.Prior to installation of this modification it must be determined thatthe interrelationship 10016107 EMS TECHNOLOGIES CANADA LTD EASA.IM.A.S.02297 TCCA STC SA05-12, ISSUE 3, DAT Installation of EMS HSD-64/-128/-X/-400/-400i/- This STC is approved only for the product HD-710 High Speed Data Transceiver configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined 10015314 EMTEQ EASA.IM.A.S.00184 FAA STC ST00221AT B727-100, B727-200 Installation of a Digital Flight Data Recorder Upgrade from 6 to 11 channels in accordance with Avitas Engineering Report No 92AMJT. 003 R-1, Revision B, dated May 4, 1993 or later 1. This approval should not be extended to other aircraft of this modelon which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this 10015315 EMTEQ EASA.IM.A.S.00185 FAA STC ST02006AT 727-100, 727-200 change and any other previously ap Installation of an Allied Signal 18 Channel Flight 1. This approval should not be extended to Data Recorder (Upgrade) for Aircraft not other aircraft of this model on which other containing a Flight Data Acquisition Unit in previously approved modifications are accordance with Avitas Engineering Report No incorporated, unless it is determined by the 99AMJT.040R-1, No Revision, dated march installer that the interrelationship between this 15, 1999, Appendix A, master Drawi change and any other previously a 10015645 EMTEQ EASA.IM.A.S.01609 REV 1 FAA STC ST02019AT B767-300 Installation of Passenger Cabin Interior Arrangement 10015316 EMTEQ ENGINEERING EASA.IM.A.S.00188 FAA STC ST02869AT BOEING 767-300 Installation of a passenger cabin interior arrangement in accordance with Master Drawing List ANST-048-MDL, Revision C dated 27/05/2004 or later EASA approved revision 10015404 EMTEQ ENGINEERING EASA.IM.A.S.01115 FAA STC ST02780AT BOEING 757-200 Installation of Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS) Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the prod 1. Subject to compliance with the provisions of Part 21 Subpart E, this STC and associated data shall remain valid until surrendered, withdrawn or otherwise terminated2. If transfer of this Certificate is requested under Part 21A.116 the STC will be 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 04/01/2013 Page 206/462 15.08.2012 27.06.2007 07.10.2004 07.10.2004 02.02.2009 01.10.2004 04.05.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015405 EMTEQ ENGINEERING EASA.IM.A.S.01116 FAA STC ST02761AT BOEING 757 Installation of Honeywell RESCU 406AF This STC is approved only for the product 05.06.2005 BOEING 767 Emergency Locator Transmitter (ELT) configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015407 EMTEQ ENGINEERING EASA.IM.A.S.01118 FAA STC ST02896AT AIRBUS A319 SERIES Installation of a Kannad Model 406-AF 1. This STC is approved only for the product 26.10.2005 AIRBUS A320 SERIES Emergency Locator Transmitter (ELT) configuration as defined in the approved design AIRBUS A321 SERIES data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015408 EMTEQ ENGINEERING EASA.IM.A.S.01122 FAA STC ST02896AT FOKKER F.28 MARK 0100 Installation of a Kannad Model 406-AF Emergency Locator Transmitter (ELT) in accordance with FAA STC ST02896AT dated 22/07/05 or later EASA-approved revision. 10.03.2006 10015566 EMTEQ ENGINEERING EASA.IM.A.S.01470 FAA STC SA03020AT BAE JETSTREAM 3101 Installation of Sandel Model ST3400 Terrain BAE JETSTREAM 3201 SERIES Awareness and Warning System (TAWS) 10015568 EMTEQ ENGINEERING EASA.IM.A.S.01475 FAA STC ST02793AT BEECH 1900D Installation of Honeywell Mk VI Enhanced 1. AFMS is required on-board for operation Ground Proximity Warning System (EGPWS). with Beechcraft 1900 D series. 10015569 EMTEQ ENGINEERING EASA.IM.A.S.01476 FAA STC ST03022AT EMBRAER EMB-120 Installation of Sandel Model ST3400 Terrain Awareness and Warning System 10015570 EMTEQ ENGINEERING EASA.IM.A.S.01477 FAA STC SA02821AT BEECH 1900D Installation of Sandel Model ST3400 Terrain RAYTHEON 1900C Awareness and Warning System 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.2. AFMS is required o 10015571 EMTEQ ENGINEERING EASA.IM.A.S.01478 FAA STC ST03003AT BOEING 767-200 Honeywell Mk V Enhanced Ground Proximity 01.12.2005 BOEING 767-300 Warning System Installation 10015638 EMTEQ ENGINEERING EASA.IM.A.S.01595 REV 1 FAA STC ST02929AT 1. BAE JETSTREAM 3101 Installation of an ARTEX Model C406-1 ELT 1. This STC is approved only for the product 12.09.2006 2. BOEING 727-100 Emergency Locator Transmitter (ELT) in configuration as defined in the approved design 3. BOEING 737-100 accordance with EMTEQ Master Drawing data referred to in the paragraph "Description". 4. BOEING 747-100 List(s) (MDL)as contained in EMTEQ Approved Compatibility with other aircraft/engine 5. BOEING 757-200 SERIES Model List (AML), Document No.2-22566-002, configurations shall be determined by the 6. BOEING 767-200 Revision G, dated 09 June 2006, or later installer.2. This approval shou 7. BOEING 777-200 SERIES 8. DC-9-10 SERIES BOEING 727-200 BOEING 737-200 BOEING 737-300 BOEING 737-400 BOEING 737-500 BOEING 737-600 BOEING 737-700 BOEING 737-800 BOEING 747-200B BOEING 747-200C BOEING 747-200F BOEING 747-300 BOEING 747-400 SERIES BOEING 747-SP BOEING 767-300 DC-9-20 SERIES DC-9-30 SERIES DC-9-40 SERIES DC-9-50 SERIES approved r 10015828 EMTEQ ENGINEERING EASA.IM.A.S.01917 FAA STC ST03212AT BOEING 737-300 SERIES Installation of an Active Noise Reduction (ANR) 23.05.2006 BOEING 737-400 SERIES BOEING 737-500 SERIES Headset 10015951 EMTEQ ENGINEERING EASA.IM.A.S.02093 FAA STC ST03269AT BAE JETSTREAM 3101 Installation of a Honeywell CAS 67A Traffic 01.08.2006 BAE JETSTREAM 3201 SERIES Alert & Collision Avoidanc System II (TCAS II) & Dual Mode S Transponder 10016111 EMTEQ ENGINEERING EASA.IM.A.S.02301 FAA STC ST03345AT BOEING 767-200 Installation of an Enhanced Surveillance None 26.02.2007 BOEING 767-300 System (EHS) to expand Transponder Mode-S functionality 10016113 EMTEQ ENGINEERING EASA.IM.A.S.02303 FAA STC ST02297AT AIRBUS A300 MODEL B2-203 This installation added three additional 21.06.2007 AIRBUS A300 MODEL B4-103 parameters to be recorded bby the existing AIRBUS A300 MODEL B4-203 Flight Data Recorder. 04/01/2013 Page 207/462 10.01.2006 01.12.2005 19.12.2005 28.11.2005
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04/01/2013 Page 1/462 - EASA

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